CA2147037C - Procede et machine pour la realisation d'une armature en forme de plaque pour une piece de matiere composite - Google Patents
Procede et machine pour la realisation d'une armature en forme de plaque pour une piece de matiere composite Download PDFInfo
- Publication number
- CA2147037C CA2147037C CA002147037A CA2147037A CA2147037C CA 2147037 C CA2147037 C CA 2147037C CA 002147037 A CA002147037 A CA 002147037A CA 2147037 A CA2147037 A CA 2147037A CA 2147037 C CA2147037 C CA 2147037C
- Authority
- CA
- Canada
- Prior art keywords
- wire
- layers
- frame
- sections
- thread
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/06—Fibrous reinforcements only
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/24—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least three directions forming a three dimensional structure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/06—Fibrous reinforcements only
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/22—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure
- B29C70/228—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure the structure being stacked in parallel layers with fibres of adjacent layers crossing at substantial angles
-
- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
- D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
- D04H3/08—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating
- D04H3/10—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with bonds between yarns or filaments made mechanically
- D04H3/115—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with bonds between yarns or filaments made mechanically by applying or inserting filamentary binding elements
-
- D—TEXTILES; PAPER
- D05—SEWING; EMBROIDERING; TUFTING
- D05B—SEWING
- D05B23/00—Sewing apparatus or machines not otherwise provided for
-
- D—TEXTILES; PAPER
- D05—SEWING; EMBROIDERING; TUFTING
- D05B—SEWING
- D05B31/00—Workpiece holders or hold-downs in machines for sewing leather
-
- D—TEXTILES; PAPER
- D05—SEWING; EMBROIDERING; TUFTING
- D05B—SEWING
- D05B29/00—Pressers; Presser feet
- D05B29/06—Presser feet
-
- D—TEXTILES; PAPER
- D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B2505/00—Industrial
- D10B2505/02—Reinforcing materials; Prepregs
Landscapes
- Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Moulding By Coating Moulds (AREA)
- Laminated Bodies (AREA)
- Reinforced Plastic Materials (AREA)
- Treatment Of Fiber Materials (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9404582 | 1994-04-18 | ||
FR9404582A FR2718757B1 (fr) | 1994-04-18 | 1994-04-18 | Procédé et machine pour la réalisation d'une armature en forme de plaque pour une pièce de matière composite. |
Publications (2)
Publication Number | Publication Date |
---|---|
CA2147037A1 CA2147037A1 (fr) | 1995-10-19 |
CA2147037C true CA2147037C (fr) | 2005-07-12 |
Family
ID=9462198
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA002147037A Expired - Fee Related CA2147037C (fr) | 1994-04-18 | 1995-04-13 | Procede et machine pour la realisation d'une armature en forme de plaque pour une piece de matiere composite |
Country Status (6)
Country | Link |
---|---|
US (1) | US5759321A (de) |
EP (1) | EP0678610B1 (de) |
JP (1) | JPH07290451A (de) |
CA (1) | CA2147037C (de) |
DE (1) | DE69510491T2 (de) |
FR (1) | FR2718757B1 (de) |
Families Citing this family (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6051089A (en) * | 1997-02-07 | 2000-04-18 | Mcdonnell Douglas Corporation | Reinforcing member for composite workpieces and associated methods |
ES2160282T3 (es) * | 1997-06-10 | 2001-11-01 | Trevira Gmbh | Un metodo y una planta para la produccion de un producto tridimensional reforzado con fibra. |
DE10005202B4 (de) * | 2000-02-03 | 2007-03-01 | Institut Für Verbundwerkstoffe Gmbh | Verfahren und Vorrichtung zur kontinuierlichen bauteil- und prozessorientierten Herstellung von Verstärkungsstruktur-Halbzeugen für Faser-Kunststoff-Verbundwerkstoffe |
FR2819804B1 (fr) * | 2001-01-24 | 2003-04-25 | Eads Launch Vehicles | Procede de fabrication d'une piece en carbone/carbone |
US6645333B2 (en) | 2001-04-06 | 2003-11-11 | Ebert Composites Corporation | Method of inserting z-axis reinforcing fibers into a composite laminate |
US7105071B2 (en) * | 2001-04-06 | 2006-09-12 | Ebert Composites Corporation | Method of inserting z-axis reinforcing fibers into a composite laminate |
US7056576B2 (en) * | 2001-04-06 | 2006-06-06 | Ebert Composites, Inc. | 3D fiber elements with high moment of inertia characteristics in composite sandwich laminates |
US7785693B2 (en) | 2001-04-06 | 2010-08-31 | Ebert Composites Corporation | Composite laminate structure |
US6676785B2 (en) * | 2001-04-06 | 2004-01-13 | Ebert Composites Corporation | Method of clinching the top and bottom ends of Z-axis fibers into the respective top and bottom surfaces of a composite laminate |
US7731046B2 (en) * | 2001-04-06 | 2010-06-08 | Ebert Composites Corporation | Composite sandwich panel and method of making same |
US20050025948A1 (en) * | 2001-04-06 | 2005-02-03 | Johnson David W. | Composite laminate reinforced with curvilinear 3-D fiber and method of making the same |
US20040005435A1 (en) * | 2001-09-08 | 2004-01-08 | Gangarao Hota V.S. | 3-Dimensionally (3-d) stitched fabrics |
FR2832738B1 (fr) * | 2001-11-27 | 2004-02-13 | Eads Launch Vehicles | Dispositif de tramage pour la realisation d'armatures textiles epaisses et armatures ainsi obtenues |
FR2835854B1 (fr) * | 2002-02-14 | 2005-12-30 | Jean Dessinges | Preformes fibreuses et leur procede de fabrication |
FR2836690B1 (fr) * | 2002-03-04 | 2004-08-27 | Eads Launch Vehicles | Procede pour la realisation d'une piece monolithique composite thermostructurale a double paroi et piece obtenue |
US20050118448A1 (en) * | 2002-12-05 | 2005-06-02 | Olin Corporation, A Corporation Of The Commonwealth Of Virginia | Laser ablation resistant copper foil |
IL163135A (en) * | 2004-07-21 | 2010-02-17 | Yair Eilam | Sewing machine for stitching with a composite thread |
FR2909920B1 (fr) * | 2006-12-15 | 2009-03-20 | Snecma Propulsion Solide Sa | Procede de realisation d'un ensemble carter-divergent |
ITMI20080971A1 (it) * | 2008-05-26 | 2009-11-27 | Nat Style Ltd | Dispositivo e procedimento di produzione in continuo di un tessuto tridimensionale per la produzione di pannelli. |
KR101319361B1 (ko) * | 2009-07-16 | 2013-10-16 | 시노마 사이언스 앤드 테크놀러지 엘티디. | 통합형 다층 직물의 형성 방법 및 그 장치 |
US9115584B2 (en) | 2012-04-24 | 2015-08-25 | General Electric Company | Resistive band for turbomachine blade |
US11701845B2 (en) * | 2019-09-17 | 2023-07-18 | Nike, Inc. | Method for forming a composite sole structure component |
Family Cites Families (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3322868A (en) * | 1963-07-02 | 1967-05-30 | Douglas Aircraft Co Inc | Three dimensional reinforced structure |
US3955602A (en) * | 1967-10-16 | 1976-05-11 | Avco Corporation | Apparatus for fabricating three-dimensional fabric material |
US3425884A (en) * | 1967-11-06 | 1969-02-04 | Crompton & Knowles Corp | Method of making an open mesh,rigid,glass fiber reinforced resin structure |
US4038440A (en) * | 1972-01-24 | 1977-07-26 | Avco Corporation | Three dimensional fabric material |
US4218276A (en) * | 1972-03-31 | 1980-08-19 | Avco Corporation | Method for making 3-D structures |
FR2355936A1 (fr) * | 1976-02-03 | 1978-01-20 | Commissariat Energie Atomique | Procede de fabrication de pieces en tissus tri-dimensionnels |
FR2395340A1 (fr) * | 1977-06-20 | 1979-01-19 | Aerospatiale | Procede et machine de tissage tridimensionnel pour la realisation d'armatures tissees de revolutions creuses |
FR2427198A1 (fr) * | 1978-06-02 | 1979-12-28 | Europ Propulsion | Texture tridimensionnelle presentant une direction privilegiee |
US4288267A (en) * | 1980-01-21 | 1981-09-08 | Mcclean Anderson, Inc. | Preliminary and end winding method and apparatus |
FR2531459A1 (fr) * | 1982-08-09 | 1984-02-10 | Aerospatiale | Procede et machine de realisation de pieces complexes par tissage multidirectionnel |
US4503788A (en) * | 1982-09-24 | 1985-03-12 | Grumman Aerospace Corporation | Translaminar stitching apparatus for composite airframe part assembly |
FR2565262B1 (fr) * | 1984-05-29 | 1986-09-26 | Europ Propulsion | Procede de fabrication d'une texture fibreuse multidirectionnelle et dispositif destine a la mise en oeuvre du procede |
FR2612950B1 (fr) * | 1987-03-25 | 1989-06-09 | Aerospatiale | Procede de fabrication d'elements d'armature composites tisses en trois dimensions, machine pour sa mise en oeuvre et produit obtenu |
DE3712013A1 (de) * | 1987-04-09 | 1988-10-27 | Vorwerk Co Interholding | Verfahren und vorrichtung zur herstellung von textilbloecken unbegrenzter dicke |
EP0484391B1 (de) * | 1989-07-25 | 1995-09-20 | Dunlop Limited | Herstellung von kohlefaser-halbfabrikaten |
US5158027A (en) * | 1991-12-19 | 1992-10-27 | Tapistron International, Inc. | Presser foot for hollow needle tufting apparatus |
FR2686627B1 (fr) * | 1992-01-24 | 1995-06-16 | Aerospatiale | Procede pour le piquage d'une piece fibreuse, piece fibreuse ainsi obtenue et piece composite fibres-matrice obtenue a partir de ladite piece fibreuse. |
FR2687173B1 (fr) * | 1992-02-11 | 1995-09-08 | Aerospatiale | Procede pour la realisation d'une armature de fibres pour piece de matiere composite, et piece composite comportant une telle armature. |
FR2705610B1 (fr) * | 1993-05-26 | 1995-08-11 | Aerospatiale | Procédé de fabrication de bielle en matériau composite monobloc par mise en place de fibres pré-imprégnées sur un mandrin extractible et bielle ainsi obtenue. |
US5468329A (en) * | 1994-03-01 | 1995-11-21 | Advanced Composites, Inc. | Universal pin strip and ring for filament winding |
-
1994
- 1994-04-18 FR FR9404582A patent/FR2718757B1/fr not_active Expired - Fee Related
-
1995
- 1995-04-03 EP EP95400730A patent/EP0678610B1/de not_active Expired - Lifetime
- 1995-04-03 DE DE69510491T patent/DE69510491T2/de not_active Expired - Lifetime
- 1995-04-13 CA CA002147037A patent/CA2147037C/fr not_active Expired - Fee Related
- 1995-04-18 JP JP7092848A patent/JPH07290451A/ja active Pending
-
1996
- 1996-07-25 US US08/686,307 patent/US5759321A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
FR2718757A1 (fr) | 1995-10-20 |
US5759321A (en) | 1998-06-02 |
DE69510491T2 (de) | 1999-11-25 |
JPH07290451A (ja) | 1995-11-07 |
CA2147037A1 (fr) | 1995-10-19 |
DE69510491D1 (de) | 1999-08-05 |
EP0678610A1 (de) | 1995-10-25 |
FR2718757B1 (fr) | 1996-06-14 |
EP0678610B1 (de) | 1999-06-30 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
EEER | Examination request | ||
MKLA | Lapsed |
Effective date: 20130415 |